// A-ST SST2010 North America by Shigeru Tanaka // Swing-wing SST2010 for Air Canada, American Airlines, // Pan American, and United Airlines [fltsim.0] title=A-ST SST2010 North America sim=A-ST SST2010 model= panel= sound= texture= checklists= ui_manufacturer=A-ST SST2010 North America ui_type=A-ST SST2010 American Airlines ui_variation=SST2010 for American Airlines description=An innovative conceptual model of Super Sonic Transport for 2010 in American Airlines livery. Futuristic design with swing-wing configuration and luxurious mach 2.3 crusing speed. Original model by Shigeru Tanaka. atc_heavy=1 atc_id=N2010AA atc_airline=American Airlines atc_flight_number=N2010 [fltsim.1] title=A-ST SST2010 North America2 sim=A-ST SST2010 model= panel= sound= texture=1 checklists= ui_manufacturer=A-ST SST2010 North America ui_type=A-ST SST2010 Pan American ui_variation=SST2010 for Pan American description=An innovative conceptual model of Super Sonic Transport for 2010 in Pan American livery. Futuristic design with swing-wing configuration and luxurious mach 2.3 crusing speed. Original model by Shigeru Tanaka. atc_heavy=1 atc_id=N2010PA atc_airline=Pan American atc_flight_number=N2010 [fltsim.2] title=A-ST SST2010 North America3 sim=A-ST SST2010 model= panel= sound= texture=2 checklists= ui_manufacturer=A-ST SST2010 North America ui_type=A-ST SST2010 Air Canada ui_variation=SST2010 de la Air Canada description=Ce modele futuriste de haute qualite, SST2010. Annee 2010, une nouvelle generation de supersonic aux couleurs de la Air Canada. Operationnelles vitesse mach 2.3. Realisation originale de Shigeru Tanaka. Bon voyage. atc_heavy=1 atc_id=C2010 atc_airline=Air Canada atc_flight_number=C2010 [fltsim.3] title=A-ST SST2010 North America4 sim=A-ST SST2010 model= panel= sound= texture=3 checklists= ui_manufacturer=A-ST SST2010 North America ui_type=A-ST SST2010 United Airlines ui_variation=SST2010 for United Airlines description=An innovative conceptual model of Super Sonic Transport for 2010 in United Airlines livery. Futuristic design with swing-wing configuration and luxurious mach 2.3 crusing speed. Original model by Shigeru Tanaka. atc_heavy=1 atc_id=N2010UA atc_airline=United Airlines atc_flight_number=N2010 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=234567.000 empty_weight_roll_MOI=10431175.000 empty_weight_pitch_MOI=22779505.000 empty_weight_yaw_MOI=19237558.000 empty_weight_coupled_MOI=1300.000 max_gross_weight=401772.195 [flight_tuning] cruise_lift_scalar=1.309317 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.309317 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [fuel] LeftMain=0.000, 0.000, 0.000, 11728.000, 0.000 LeftAux=0.000, -53.333, 0.000, 750.000, 0.000 RightMain=0.000, 0.000, 0.000, 11728.000, 0.000 RightAux=0.000, 53.333, 0.000, 750.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=2886.000 wing_span=133.417 wing_root_chord=21.667 wing_dihedral=6.998 wing_incidence=0.000 wing_twist=-1.000 oswald_efficiency_factor=0.750 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=1400.000 htail_span=41.667 htail_pos_lon=-83.333 htail_pos_vert=0.000 htail_incidence=0.000 htail_sweep=0.000 vtail_area=700.000 vtail_span=30.166 vtail_sweep=0.000 vtail_pos_lon=-66.667 vtail_pos_vert=5.833 elevator_area=350.000 aileron_area=115.440 rudder_area=119.000 elevator_up_limit=15.502 elevator_down_limit=10.626 aileron_up_limit=19.481 aileron_down_limit=14.897 rudder_limit=23.491 elevator_trim_limit=9.481 spoiler_limit=59.989 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] point.0=1.000, 48.77, 0.000, -17.0346, 1781.803, 0.000, 3.285, 64.680, 0.470, 2.5, 0.7470, 6.9, 6.9, 0, 0.0, 250.0 point.1=1.000, -40.417, -11.167, -16.746, 1574.803, 1.000, 3.285, 0.000, 0.470, 2.5, 0.7470, 6.9, 6.9, 2, 0.0, 250.0 point.2=1.000, -40.417, 11.167, -16.746, 1574.803, 2.000, 3.285, 0.000, 0.470, 2.5, 0.7470, 6.9, 6.9, 3, 0.0, 250.0 point.3=2.000, -52.417, -58.417, -3.417, 1274.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4=2.000, -52.417, 58.417, -3.417, 1274.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5=2.000, 101.167, 0.000, -2.667, 1504.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.6=2.000, -78.000, 0.000, -4.867, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch=0.00000007 static_cg_height=16.557 gear_system_type=0 [GeneralEngineData] engine_type=1 Engine.0=-6.250, -13.950, -3.417 Engine.1=-8.333, -20.333, -4.833 Engine.2=-8.333, 20.333, -4.833 Engine.3=-6.250, 13.950, -3.417 fuel_flow_scalar=1.000 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002 inlet_area=59.990 rated_N2_rpm=29920.000 static_thrust=53991.300 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.0 [Reference Speeds] flaps_up_stall_speed=123.000 full_flaps_stall_speed=98.400 cruise_speed=2392.420 max_indicated_speed=1207.187500 max_mach=2.300 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=83.495, 0.000, 7.395 [General] performance=Designer: Shigeru Tanaka\nModel file: sstnoam.zip\nCopyright: Shigeru Tanaka\nProject: March 1, 2003\nEmail: wing.shigeru@nifty.ne.jp\nCopyright held lawfully by the author under the copyright laws applicable and concerned:\nDigital watermarking is the technology wherein copyright owner's identification information, copyright control information and the similar are embedded into digitally created data in such manner as not to be easily perceived, thereafter watermarking information is detected from the data at necessity, thereby copyright control and protection is duly conducted and effectively promoted.\nCopyright 2003 Shigeru Tanaka atc_type= atc_model= [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000 pitch_takeoff_ga=8.000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -13, -27.06, -3.5, fx_navredh , light.1=3, -13, 27.06, -3.5, fx_navgreh , light.2=3, -101, 0.00, 5.3, fx_navwhih , light.3=2, 17, -4.5, -3.7, fx_navwhih , light.4=2, 17, 4.5, -3.7, fx_navwhih , light.5=2, -85, 0.00, 22, fx_strobeh , light.6=1, 30.05, 0.00, 5.8, fx_beaconh , light.7=1, -20.22, 0.00, -5.9, fx_beaconb , light.8=4, -16.24, 0.00, 9.19, fx_vclighth, [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [SMOKESYSTEM] smoke.0=-24.00,-70.00,20.00, fx_sst2010smoke smoke.1=-24.00,-65.00,14.00, fx_sst2010smoke smoke.2=2.00,-65.00,-14.00, fx_sst2010smoke smoke.3=3.00,-70.00,-20.00, fx_sst2010smoke smoke.4=-212.00,0,-150.00,20.00, fx_sst2010smoke_special smoke.5=-323.00,0,-145.00,14.00, fx_sst2010smoke_original smoke.6=178.00,0,-145.00,-14.00, fx_sst2010smoke_novel smoke.7=236.00,0,-150.00,-20.00, fx_sst2010smoke_innovative smoke.8=-128,-64.875,20.0000,fx_sst2010afterburner smoke.9=-229,-66.75,20.0000,fx_sst2010afterburner_special smoke.10=-330,-64.875,14.500,fx_sst2010afterburner smoke.11=-431,-66.75,14.500,fx_sst2010afterburner_original smoke.12=-532,-64.875,-14.500,fx_sst2010afterburner smoke.13=-633,-66.75,-14.500,fx_sst2010afterburner_novel smoke.14=-734,-64.875,-20.00,fx_sst2010afterburner smoke.15=-835,-66.650,-20.00,fx_sst2010afterburner_innovative smoke.100=0, 007, 0.007, -0.007, Marlboro Long Size [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [direction_indicators] direction_indicator.0=3,0 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=0 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=2.999, 0.000 flaps-position.2=6.198, 0.000 flaps-position.3=9.997, 0.000 flaps-position.4=11.996, 0.000 flaps-position.5=14.995, 0.000 flaps-position.6=17.994, 0.000 flaps-position.7=20.993, 0.000 flaps-position.8=24.992, 0.000 [brakes] toe_brakes_scale=2.731 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [ALCHOLESYSTEM] whisky.0=0.07, 1048.71, 28.05, Canadian Whisky Crown Royal whisky.1=0.08, 1048.72, 27.05, Tennessee Whisky Jack Daniel's [Humor system] type=2 powered by Shigeru Tanaka
